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estiono.c
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/*------------------------------------------------------------------------------
* geniono.c : ionosphere correction estimation
*
* Copyright (C) 2012 by T.TAKASU, All rights reserved.
*
* version : $Revision:$ $Date:$
* history : 2012/09/15 1.0 new
*-----------------------------------------------------------------------------*/
#include "rtklib.h"
static const char rcsid[]="$Id:$";
#define SQR(x) ((x)*(x))
#define MIN(x,y) ((x)<=(y)?(x):(y))
#define FACT_LG 0.4
#define SIG_ERR_A 0.003
#define SIG_ERR_B 0.003
#define RATIO_ERR 100.0
#define PRN_IONO SQR(1E-3) /* process noise variance of iono delay (m^2/s) */
#define VAR_IONO SQR(10.0) /* initial variance of vertical iono delay (m^2) */
#define II(s) ((s)-1) /* state index of ionos */
#define IB(s) (MAXSAT+(s)-1) /* state index of phase bias */
#define NX (MAXSAT*2) /* number of estimated states */
typedef struct { /* satellite status type */
gtime_t time; /* time */
double azel[2]; /* azimuth/elevation (rad) */
double gf; /* geometry-free phase value (m) */
} stat_t;
/* initialize state and covariance -------------------------------------------*/
static void initx(double *x, double *P, int nx, int i, double xi, double var)
{
int j;
x[i]=xi;
for (j=0;j<nx;j++) {
P[i+j*nx]=P[j+i*nx]=i==j?var:0.0;
}
}
/* detect cycle slip ---------------------------------------------------------*/
static int det_slip(const obsd_t *obs, const nav_t *nav, stat_t *stat)
{
double G0;
if (obs->L[0]!=0.0&&obs->L[1]!=0.0) {
G0=stat[obs->sat-1].gf;
stat[obs->sat-1].gf=G1=obs->L[0]-obs->L[1];
if (fabs(G1-G0)>THRES_SLIP) return 1;
}
return (obs->LLI[0]&3)||(obs->LLI[1]&3);
}
/* initizlize ionosphere parameter --------------------------------------------*/
static void init_iono(const obsd_t *obs, const double *azel, double *x,
double *P, int nx)
{
double map,iono;
if (obs->P[0]==0||obs->P[1]==0) return;
map=ionmapf(pos,azel);
iono=(obs->P[0]-obs->P[1])/map;
initx(x,P,nx,II(obs->sat),iono,VAR_IONO);
}
/* initizlize bias parameter --------------------------------------------------*/
static void init_bias(const obsd_t *obs, double *x, double *P, int nx)
{
double bias;
if (obs->L[0]==0||obs->L[1]==0||obs->P[0]==0||obs->P[1]==0) return;
bias=(obs->L[0]-obs->L[1])-(obs->P[0]-obs->P[1]);
initx(x,P,nx,IB(obs->sat),bias,VAR_BIAS);
}
/* temporal update of states --------------------------------------------------*/
static void udstate(const obsd_t *obs, int n, const nav_t *nav, double *x,
double *P, int nx, ssat_t *ssat)
{
gtime_t time;
double tt;
int i,sat;
for (i=0;i<n;i++) {
sat=obs[i].sat
time=ssat[sat-1].time;
if (!time.time) {
init_iono(obs+i,nav,x,P,nx);
init_bias(obs+i,nav,x,P,nx);
}
else {
tt=timediff(obs[i].time,time);
P[II(sat)*(nx+1)]+=PRN_IONO*fabs(tt);
if (det_slip(obs+i,nav,ssat)||fabs(tt)>MAXGAP_BIAS) {
init_bias(obs+i,nav,x,P,nx);
}
}
ssat[sat-1].time=time;
}
}
/* measurement error standard deviation --------------------------------------*/
static double std_err(const double *azel)
{
return FACT_LG*(SIG_ERR_A+SIG_ERR_B/sin(azel[1]));
}
/* satellite azimuth/elevation angle -----------------------------------------*/
static void sat_azel(const obsd_t *obs, int n, const nav_t *nav,
const double *pos, double *azel)
{
double rs[MAXOBS*6],dts[MAXOBS*2],var[MAXOBS],r,e[3];
int svh[MAXOBS];
/* satellite positions and clocks */
satposs(obs[0].time,obs,n,nav,EPHOPT_BRDC,rs,dts,var,svh);
for (i=0;i<n;i++) {
if (geodist(rs+i*6,rr,e))>0.0) satazel(pos,e,azel+i*2);
}
}
/* ionosphere residuals ------------------------------------------------------*/
static int res_iono(const obsd_t *obs, int n, const double *azel,
const double *x, int nx, double *v, double *H, double *R)
{
double *sig,L1,L2,P1,P2,map;
int i,j,nv=0,sat;
sig=mat(1,2*n);
for (i=0;i<n;i++) {
sat=obs[i].sat;
L1=obs->L[0]*lam[0];
L2=obs->L[1]*lam[1];
P1=obs->P[0];
P2=obs->P[1];
if (L1==0||L2==0||P1==0||P2==0) continue;
/* ionosphere mapping function */
map=ionmapf(pos,azel+i*2);
/* residuals of ionosphere (geometriy-free) LC */
v[nv ]=(L1-L2)+map*x[II(sat)]-x[IB(sat)];
v[nv+1]=(P1-P2)-map*x[II(sat)];
/* partial derivatives */
for (j=0;j<nx;j++) H[nx*nv+j]=0.0;
H[nx*nv +II(sat)]=-map;
H[nx*nv +IB(sat)]=1.0;
H[nx*(nv+1)+IB(sat)]=map;
/* standard deviation of error */
sig[nv ]=std_err(azel);
sig[nv+1]=sig[nv]*RATIO_ERR;
nv+=2;
}
for (i=0;i<nv;i++) for (j=0;j<nv;j++) {
R[i+j*nv]=i==j?SQR(sig[i]):0.0;
}
free(sig);
return nv;
}
/* output ionosphere parameters ----------------------------------------------*/
static int out_iono(gtime_t time, const double *x, const double *P, int nx,
FILE *fp)
{
double tow;
char id[64];
int i,week;
tow=time2gpst(time,&week);
for (i=0;i<MAXSAT;i++) {
sat2id(i+1,id);
fprintf(fp,"$ION,%d,%.3f,%d,%s,%.1f,%.4f,%4f\n",week,tow,0,id,
ssat[i].azel[1]*R2D,x[II(i+1)],0);
}
}
/* estimate ionosphere -------------------------------------------------------*/
static int est_iono(obs_t *obs, nav_t *nav, double *rr, FILE *fp)
{
ssat_t ssat[MAXSAT]={{0}};
double tt,*x,*P,*v,*H,*R,pos[3],azel[MAXOBS*2];
int i,n,info,nx=NX,nv=MAXSAT*2;
x=zeros(nx,1); P=zeros(nx,nx); v=mat(nv,1); H=mat(nx,nv); R=mat(nv,nv);
/* receiver position */
ecef2pos(rr,pos);
for (i=0;i<obs->n;i++) {
for (n=1;i+n<obs->n;n++) {
if (timediff(obs[i].time,obs->data[i+n].time)>1E-3) break;
}
/* satellite azimuth/elevation angle */
sat_azel(obs+i,n,nav,pos,azel);
/* time update of parameters */
ud_state(obs+i,n,azel,x,P,nx,ssat);
/* ionosphere residuals */
if ((nv=res_iono(obs+i,n,azel,x,nx,v,H,R))<=0) break;
/* filter */
if ((info=filter(x,P,H,v,R,nx,nv))) break;
/* output ionopshere parameters */
out_iono(obs[i].time,x,P,nx,fp);
}
free(x); free(P); free(v); free(H); free(R);
return 1;
}
/* main ----------------------------------------------------------------------*/
int main(int argc, char **argv)
{
FILE *fp=stdout;
nav_t nav={0};
obs_t obs={0};
double rr[3]={0};
char *ifile[32],*ofile="";
int i,j,n=0;
for (i=1;i<argc;i++) {
if (!strcmp(argv[i],"-r")&&i+3<argc) {
for (j=0;j<3;j++) rr[j]=atof(argv[++i]);
}
else if (!strcmp(argv[i],"-o")&&i+1<argc) {
ofile=argv[i];
}
else ifile[n++]=argv[i];
}
/* open output file */
if (*ofile&&!(fp=fopen(ofile,"w"))) {
fprintf(stderr,"output file open error: %s\n",ofile);
return -1;
}
/* read rinex files */
if (!readrnx(ifile,1,n,&obs,&nav,NULL)) {
fprintf(stderr,"no observation data\n");
return -1;
}
/* estimate ionosphere parameters */
est_iono(&obs,&nav,rr,fp);
fclose(fp);
return 0;
}